US20020136847A1 - Double tapered article - Google Patents
Double tapered article Download PDFInfo
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- US20020136847A1 US20020136847A1 US09/812,933 US81293301A US2002136847A1 US 20020136847 A1 US20020136847 A1 US 20020136847A1 US 81293301 A US81293301 A US 81293301A US 2002136847 A1 US2002136847 A1 US 2002136847A1
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- Prior art keywords
- mandrel
- rigid
- passage
- shaft
- flexible
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Links
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- 238000000034 method Methods 0.000 claims abstract description 38
- RZSCFTDHFNHMOR-UHFFFAOYSA-N n-(2,4-difluorophenyl)-2-[3-(trifluoromethyl)phenoxy]pyridine-3-carboxamide;1,1-dimethyl-3-(4-propan-2-ylphenyl)urea Chemical compound CC(C)C1=CC=C(NC(=O)N(C)C)C=C1.FC1=CC(F)=CC=C1NC(=O)C1=CC=CN=C1OC1=CC=CC(C(F)(F)F)=C1 RZSCFTDHFNHMOR-UHFFFAOYSA-N 0.000 claims description 24
- 239000004744 fabric Substances 0.000 claims description 15
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- 229920000647 polyepoxide Polymers 0.000 claims description 8
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Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B1/00—Layered products having a non-planar shape
- B32B1/08—Tubular products
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B65/00—Implements for throwing ; Mechanical projectors, e.g. using spring force
- A63B65/02—Spears or the like ; Javelins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
- B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/82—Cores or mandrels
- B29C53/821—Mandrels especially adapted for winding and joining
- B29C53/824—Mandrels especially adapted for winding and joining collapsible, e.g. elastic or inflatable; with removable parts, e.g. for regular shaped, straight tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/583—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features
- B29C53/585—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features the cross-section varying along their axis, e.g. tapered, with ribs, or threads, with socket-ends
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/52—Sports equipment ; Games; Articles for amusement; Toys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2363/00—Epoxy resins
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31511—Of epoxy ether
Definitions
- the present invention relates to a method of forming a molded article and, more particularly, to a method of forming and a molded article having a passage therein which has a cross-sectional dimension adjacent an end which is less than at a location which is spaced from that end.
- Double tapered articles are known in which the cross-sectional dimension of the article, e.g. the diameter, decreases toward each of the ends.
- These are typically articles of metal or other materials which are formed by grinding or sanding the ends of a rod to define the decreasing cross-sectional dimension and/or by compressing or swaging a tube toward one or both of its ends to form at least one and sometimes opposite tapered ends.
- Such compressing or swaging of tubing is, for example, disclosed in my U.S. Pat. No. 3,274,816.
- Such shafts of varying internal cross-sectional dimensions would be highly desirable, for example, in a javelin where the cross-sectional dimensions of both the interior and exterior of the shaft desirably vary over the length of the javelin for proper weight, balance and flexing qualities.
- the present invention makes it possible to form a one piece, molded, polymeric shaft having a passage therethrough which is formed by the mold, and which varies in cross-sectional dimension over its length so that these dimensions are less at the ends of the shaft than at a location spaced from the ends. Yet the mold about which the shaft has been formed is capable of easy removal from such shaft passage after the article has been formed and set.
- a method of forming a molded article having a passage therein which has a cross-sectional dimension adjacent an end which is less than at a location which is spaced from such end comprises providing an elongate substantially rigid mandrel having a substantially rigid surface thereon and which surface has a given shape, and covering a substantial portion of the rigid surface of the rigid mandrel with a flexible mandrel.
- the flexible mandrel has an inner surface which assumes the shape of the rigid surface of the rigid mandrel when the flexible mandrel is positioned thereon, and an exterior surface on the flexible mandrel which has a cross-sectional dimension which is less adjacent an end thereof than at a location which is spaced from the end.
- the flexible mandrel is covered with a material which is to form the molded article, with the rigid and flexible mandrels defining a mold about which the molded article is formed by the material.
- the material is set to form the molded article about the mandrels with the mandrels defining the passage in the molded article, and the mandrels are removed from the molded article from the end of the passage which has the cross-sectional dimension which is less than at the location which is spaced from such end.
- the rigid mandrel is removed from the passage first and then the flexible mandrel is removed from the passage.
- the rigid mandrel is metal
- the rigid mandrel is an elongate solid rod.
- the rigid mandrel is elongate and of uniform cross-sectional dimension over a major portion of its length, and is preferably cylindrical.
- the flexible mandrel stretches when it is being removed from the passage in the molded article.
- the flexible mandrel is formed of silicone rubber.
- the flexible mandrel is a sleeve which is pulled over the rigid mandrel to cover its rigid surface.
- the flexible mandrel has a high thermal coefficient of expansion so that it exerts a pressure on the wall of the passage and the rigid surface of the rigid mandrel during the setting of the material.
- the material is heated during setting.
- the material is constrained on the side thereof opposite the mandrels during setting.
- the material is constrained by wrapping with a tight stretch film.
- the material includes an epoxy resin.
- the method is for molding the shaft of a javelin.
- an article of manufacture comprises a molded elongate single piece shaft formed of a polymeric material with the shaft having first and second ends.
- a passage opens to the first end and extends from the first end toward the second end and over a substantial portion of the length of the elongate shaft.
- the passage is formed from and defined by the mold upon which the shaft is molded and after the mold is removed, and the passage has a cross-sectional dimension which is less at the first and second ends than between the ends.
- the shaft also has an external surface having a cross-sectional dimension which is less at the first and second ends than between the ends.
- the polymeric material includes an epoxy resin.
- the polymeric material comprises a fabric selected from the group consisting essentially of fiberglass, carbon fibers, ceramic fibers and mixtures thereof which is impregnated with an epoxy resin.
- the shaft is the shaft of a javelin.
- FIG. 1 is a cross-sectioned side elevation view of a double tapered shaft, such as a javelin shaft, being formed by the preferred method of the present invention
- FIG. 2 is a broken, enlarged side elevational cross-sectioned view of the right end of the shaft as seen in FIG. 1, and with rigid and flexible mandrels in the position that they assume during molding as in the preferred method of the present invention;
- FIG. 3 is a view similar to FIG. 2, but showing the rigid mandrel being removed following the molding process
- FIG. 4 is a view similar to FIG. 3, but showing the flexible mandrel being removed after the rigid mandrel has been removed;
- FIG. 5 is an enlarged, broken side elevation view of the shaft of FIG. 1 after the mandrels have been removed and with a javelin tip installed on the right end of the shaft;
- FIG. 6 is a perspective view of a completed javelin formed from the shaft of the present invention and with a javelin tip and hand grip positioned thereon.
- An inner rigid mandrel 10 comprises an elongate rod of generally uniform cross-sectional dimension over a major portion of its length.
- the rigid mandrel 10 is preferably formed of metal, is solid and is cylindrical over a major portion of its length, except for a tail portion 12 which tapers over a portion of its length as seen in FIGS. 1 and 3.
- the tapered tail may be formed by grinding.
- the rigid mandrel 10 may be formed of a tube in which case the tapered tail may be formed by swaging as described in my aforementioned patent.
- the metal of the rigid mandrel 10 is preferably aluminum or steel of either the stainless or carbon variety. After forming a new rigid mandrel 10 it is preferably seasoned by coating its exterior rigid surface 16 with melted paraffin which is allowed to solidify. The mandrel is then heated again until the coating melts and drips from the rigid mandrel and the surface is then wiped dry with a soft cloth while still hot and polished after coating. After this initial seasoning and prior to use, the rigid mandrel 10 is waxed with a suitable wax. These treatments permit easy removal of the rigid mandrel after the molding of the article.
- the second mandrel of the mold is a flexible mandrel 14 which is formed of a flexible, stretchable material, such as silicone rubber.
- the material of the flexible mandrel preferably has a high thermal coefficient of expansion so that when it is heated, it tends to expand somewhat to exert a pressure on the rigid surface 16 of the rigid mandrel 10 and the inner surface of the article which is to be formed by the molding process during the setting of the material of the article as will be described in further detail later.
- An example of a suitable silicon rubber with such coefficient of expansion is SE 875 with catalyst available from General Electric.
- the flexible mandrel 14 takes the form of a tubular sleeve which in use is slid over the rigid surface 16 of the rigid mandrel 10 until the end 18 of the flexible mandrel is located slightly short of the end 20 of the rigid mandrel. This permits a small portion of the length of the rigid mandrel 10 to be exposed adjacent its end 20 beyond the end 18 of the flexible mandrel, as seen in FIGS. 1 and 2, so that the rigid mandrel may be grasped to remove it from the molded article and the flexible mandrel 14 after molding.
- the flexible mandrel 14 preferably has a length which is the sum of the lengths of sections a+b+c as shown in FIG. 1.
- the external diameter of the flexible mandrel 14 over the length of section a is preferably uniform and does not vary.
- the external diameter of the flexible mandrel 14 over the length of section b does vary in accordance with the invention so that its external cross-sectional dimension or diameter adjacent section a is less than its cross-sectional external dimension or diameter adjacent the right end of section c as viewed in FIG. 1.
- the external cross-sectional dimension or diameter of the flexible mandrel 14 then preferably decreases over the length of section c, as viewed in FIG.
- the internal cross-sectional dimension or diameter of the flexible mandrel 14 tubular sleeve is preferably substantially constant over the length of sections a, b and c because the rigid mandrel 10 is substantially cylindrical and, therefore, constant in those sections.
- the increasing cross-sectional dimension or diameter of the flexible mandrel 14 over section b and the decreasing cross-sectional dimension or diameter over section c is an important feature of the invention because it achieves a principal part of the double taper of the molded article of the invention.
- the varying tapered sections and cross-sectional dimensions or diameters of the flexible mandrel 14 may be achieved either by molding the flexible mandrel with these varying dimensions or by sliding a sleeve of the flexible mandrel material over the rigid mandrel 10 and then sanding or grinding down the exterior surface of the sleeve toward the ends of the sleeve to achieve the varying cross-sectional dimension or diameter.
- the flexible mandrel 14 is first assembled upon the rigid mandrel 10 by slipping it over the conditioned and waxed rigid surface 16 of the rigid mandrel until the end 18 of the flexible mandrel assumes the position spaced slightly from the end 20 of the rigid mandrel 10 as seen in FIGS. 1 and 2.
- the flexible mandrel 14 In preferred form once the flexible mandrel 14 is positioned upon the rigid mandrel 10 , it will cover and conform to the rigid surface 16 of the rigid mandrel, will extend over the lengths of sections a, b and c as shown in FIG. 1, and will terminate before the beginning of section d. Only the tapered tail 12 of the rigid mandrel 10 will be present and exposed over the length of section d. Finally, there will be no mandrel over the length of section e, as shown in FIG. 1.
- Assembly of the molded article A may now be commenced. This is typically done by wrapping a pre-impregnated cloth or tape material 22 , as depicted in dot and dash in FIGS. 1 and 2, back and forth over the length of the mandrels. However, the impregnated cloth wrapping is preferably terminated at 24 just short of the right end 18 of the flexible mandrel 14 as viewed in FIGS. 1 and 2 to permit the exposure of a short portion of the length of the flexible mandrel to facilitate its removal once the molding operation is completed.
- the impregnated cloth or tape 22 is preferably impregnated with a thermosetting resin, and most preferably an epoxy resin which may be cured by heat.
- the tape itself may be woven or be fibers of fiberglass, carbon or ceramic in the form of a fabric.
- Suitable examples of preimpregnated fiberglass cloth or tape include MXB7409/1557 or MXB7409/7576, and of preimpregnatetd unidirectional carbon fiber tape include HYE949b, all available from Cytec Fiberite, Inc. Each of these has a cure temperature of 250° F.
- the article thus far assembled is then wrapped preferably with a tight stretch film wrapping 26 over its length, and as depicted in dot and dash in FIGS. 1 and 2.
- the stretch film wrap 26 constrains the resin impregnated cloth 22 during setting and curing. Because the flexible mandrel 14 is formed of a material which has a high thermal coefficient of expansion and the surface 16 of the rigid mandrel 10 itself is rigid, pressure will be exerted upon the inner surface of the resin impregnated cloth 22 during curing.
- the entire assembly is now heated to a temperature sufficient to cure the resin in the resin impregnated cloth 22 .
- the rigid mandrel 10 may be easily removed from the flexible mandrel 14 , as seen in FIG. 3, through the opening which is formed in the end 24 of the article A. Removal of the rigid mandrel 10 is simplified because it is of a uniform cross-sectional dimension over most of its length. Where it is not of uniform cross-sectional dimension at its tapered tail 12 , its cross-sectional dimension is diminishing which does not impede removal.
- the flexible mandrel 14 may now relax slightly away from the inner wall 28 of the passage 30 which has been formed by the mandrels during the molding process, as seen in FIG. 4. Furthermore, when the flexible mandrel 14 is pulled to remove it from the passage 30 in the direction of the arrow as seen in FIG. 4, it may further stretch somewhat which also tends to reduce its cross-sectional dimension or diameter to further simplify the removal of the flexible mandrel from the opening in the end 24 of the article A.
- the removal of the flexible mandrel 14 may be easily performed even though the diameter or cross-sectional dimension of the opening and the passage 30 is less at the end 24 than at a location to the left of the end 24 of the passage 30 as viewed in FIG. 4.
- the flexible mandrel 14 may relax somewhat away from the inner wall 28 of passage 30 when the rigid mandrel 10 is removed and/or when it is pulled to remove it, it preferably retains sufficient body to generally maintain its original shape and does not just collapse.
- one such article A which may be molded in accordance with the principles of the present invention, is the shaft of a javelin which is tapered toward each end of the shaft.
- the method of the present invention makes it possible to form a javelin shaft of a one piece composite polymeric material by molding which was not heretofore possible.
- the tail tip of the shaft at the left end of section e, as viewed in FIG. 1, is preferably cut off to form the tail of the javelin, and the right end 24 is trimmed as necessary to remove any ragged edges.
- a hollow javelin point 32 of steel or aluminum is then press fit onto the tapering end 24 of the javelin shaft A, and a hand grip 34 preferably of wrapped cotton cord, is formed intermediate the ends of the javelin and at approximately the center of gravity of the javelin.
- the method of forming the molded composite polymeric one piece article of the present invention is particularly advantageous in the making of a javelin shaft. This is because the competition specifications of a javelin are quite rigid and the double tapers, their sizing and location are advantageously considered in the weight and balance of the javelin, its mass and ability to flex.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
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Abstract
Description
- The present invention relates to a method of forming a molded article and, more particularly, to a method of forming and a molded article having a passage therein which has a cross-sectional dimension adjacent an end which is less than at a location which is spaced from that end.
- Double tapered articles are known in which the cross-sectional dimension of the article, e.g. the diameter, decreases toward each of the ends. These are typically articles of metal or other materials which are formed by grinding or sanding the ends of a rod to define the decreasing cross-sectional dimension and/or by compressing or swaging a tube toward one or both of its ends to form at least one and sometimes opposite tapered ends. Such compressing or swaging of tubing is, for example, disclosed in my U.S. Pat. No. 3,274,816.
- In certain circumstances it would be advantageous to form an elongate one piece shaft by the molding of a composite polymeric material about a mold and in which the mold, and hence the passage in the shaft which remains after the removal of the mold, has a double taper, e.g. is tapered toward each end. However, this previously has not been possible because it was not possible to remove the mold about which the shaft was formed once the polymeric material used to form the shaft has been set or cured. This is because the cross-sectional dimensions at the tapered ends of the passage which is formed by the mold are smaller than in between the ends and, therefore, block the movement of the mold, which has a larger cross-sectional dimension between its ends, out of the passage. Such shafts of varying internal cross-sectional dimensions would be highly desirable, for example, in a javelin where the cross-sectional dimensions of both the interior and exterior of the shaft desirably vary over the length of the javelin for proper weight, balance and flexing qualities.
- This problem has been solved in the present invention. The present invention makes it possible to form a one piece, molded, polymeric shaft having a passage therethrough which is formed by the mold, and which varies in cross-sectional dimension over its length so that these dimensions are less at the ends of the shaft than at a location spaced from the ends. Yet the mold about which the shaft has been formed is capable of easy removal from such shaft passage after the article has been formed and set.
- In one principal aspect of the present invention, a method of forming a molded article having a passage therein which has a cross-sectional dimension adjacent an end which is less than at a location which is spaced from such end, comprises providing an elongate substantially rigid mandrel having a substantially rigid surface thereon and which surface has a given shape, and covering a substantial portion of the rigid surface of the rigid mandrel with a flexible mandrel. The flexible mandrel has an inner surface which assumes the shape of the rigid surface of the rigid mandrel when the flexible mandrel is positioned thereon, and an exterior surface on the flexible mandrel which has a cross-sectional dimension which is less adjacent an end thereof than at a location which is spaced from the end. The flexible mandrel is covered with a material which is to form the molded article, with the rigid and flexible mandrels defining a mold about which the molded article is formed by the material. The material is set to form the molded article about the mandrels with the mandrels defining the passage in the molded article, and the mandrels are removed from the molded article from the end of the passage which has the cross-sectional dimension which is less than at the location which is spaced from such end.
- In another principal aspect of the present invention, the rigid mandrel is removed from the passage first and then the flexible mandrel is removed from the passage.
- In still another principal aspect of the present invention, the rigid mandrel is metal.
- In still another principal aspect of the present invention, the rigid mandrel is an elongate solid rod.
- In still another principal aspect of the present invention, the rigid mandrel is elongate and of uniform cross-sectional dimension over a major portion of its length, and is preferably cylindrical.
- In still another principal aspect of the present invention, the flexible mandrel stretches when it is being removed from the passage in the molded article.
- In still another principal aspect of the present invention, the flexible mandrel is formed of silicone rubber.
- In still another principal aspect of the present invention, the flexible mandrel is a sleeve which is pulled over the rigid mandrel to cover its rigid surface.
- In still another principal aspect of the present invention, the flexible mandrel has a high thermal coefficient of expansion so that it exerts a pressure on the wall of the passage and the rigid surface of the rigid mandrel during the setting of the material.
- In still another principal aspect of the present invention, the material is heated during setting.
- In still another principal aspect of the present invention, the material is constrained on the side thereof opposite the mandrels during setting.
- In still another principal aspect of the present invention, the material is constrained by wrapping with a tight stretch film.
- In still another principal aspect of the present invention, the material includes an epoxy resin.
- In still another principal aspect of the invention, the method is for molding the shaft of a javelin.
- In still another principal aspect of the present invention, an article of manufacture comprises a molded elongate single piece shaft formed of a polymeric material with the shaft having first and second ends. A passage opens to the first end and extends from the first end toward the second end and over a substantial portion of the length of the elongate shaft. The passage is formed from and defined by the mold upon which the shaft is molded and after the mold is removed, and the passage has a cross-sectional dimension which is less at the first and second ends than between the ends.
- In still another principal aspect of the present invention, the shaft also has an external surface having a cross-sectional dimension which is less at the first and second ends than between the ends.
- In still another principal aspect of the present invention, the polymeric material includes an epoxy resin.
- In still another principal aspect of the present invention, the polymeric material comprises a fabric selected from the group consisting essentially of fiberglass, carbon fibers, ceramic fibers and mixtures thereof which is impregnated with an epoxy resin.
- In still another principal aspect of the present invention, the shaft is the shaft of a javelin.
- These and other objects, features and advantages of the present invention will be more clearly understood through a consideration of the following detailed description.
- In the course of this description, reference will frequently be made to the attached drawings in which:
- FIG. 1 is a cross-sectioned side elevation view of a double tapered shaft, such as a javelin shaft, being formed by the preferred method of the present invention;
- FIG. 2 is a broken, enlarged side elevational cross-sectioned view of the right end of the shaft as seen in FIG. 1, and with rigid and flexible mandrels in the position that they assume during molding as in the preferred method of the present invention;
- FIG. 3 is a view similar to FIG. 2, but showing the rigid mandrel being removed following the molding process;
- FIG. 4 is a view similar to FIG. 3, but showing the flexible mandrel being removed after the rigid mandrel has been removed;
- FIG. 5 is an enlarged, broken side elevation view of the shaft of FIG. 1 after the mandrels have been removed and with a javelin tip installed on the right end of the shaft; and
- FIG. 6 is a perspective view of a completed javelin formed from the shaft of the present invention and with a javelin tip and hand grip positioned thereon.
- A preferred embodiment of method of forming a molded article and the molded article itself in the form of a javelin constructed in accordance with the principles of the present invention are shown in the drawings.
- As seen in FIGS. 1 and 2, a pair of mandrels are provided to form a mold about which the molded article of the invention is formed. An inner
rigid mandrel 10 comprises an elongate rod of generally uniform cross-sectional dimension over a major portion of its length. Therigid mandrel 10 is preferably formed of metal, is solid and is cylindrical over a major portion of its length, except for atail portion 12 which tapers over a portion of its length as seen in FIGS. 1 and 3. Where the rigid mandrel is a solid rod, the tapered tail may be formed by grinding. In the alternative, therigid mandrel 10 may be formed of a tube in which case the tapered tail may be formed by swaging as described in my aforementioned patent. - The metal of the
rigid mandrel 10 is preferably aluminum or steel of either the stainless or carbon variety. After forming a newrigid mandrel 10 it is preferably seasoned by coating its exteriorrigid surface 16 with melted paraffin which is allowed to solidify. The mandrel is then heated again until the coating melts and drips from the rigid mandrel and the surface is then wiped dry with a soft cloth while still hot and polished after coating. After this initial seasoning and prior to use, therigid mandrel 10 is waxed with a suitable wax. These treatments permit easy removal of the rigid mandrel after the molding of the article. - The second mandrel of the mold is a
flexible mandrel 14 which is formed of a flexible, stretchable material, such as silicone rubber. The material of the flexible mandrel preferably has a high thermal coefficient of expansion so that when it is heated, it tends to expand somewhat to exert a pressure on therigid surface 16 of therigid mandrel 10 and the inner surface of the article which is to be formed by the molding process during the setting of the material of the article as will be described in further detail later. An example of a suitable silicon rubber with such coefficient of expansion is SE 875 with catalyst available from General Electric. - The
flexible mandrel 14 takes the form of a tubular sleeve which in use is slid over therigid surface 16 of therigid mandrel 10 until theend 18 of the flexible mandrel is located slightly short of theend 20 of the rigid mandrel. This permits a small portion of the length of therigid mandrel 10 to be exposed adjacent itsend 20 beyond theend 18 of the flexible mandrel, as seen in FIGS. 1 and 2, so that the rigid mandrel may be grasped to remove it from the molded article and theflexible mandrel 14 after molding. - The
flexible mandrel 14 preferably has a length which is the sum of the lengths of sections a+b+c as shown in FIG. 1. The external diameter of theflexible mandrel 14 over the length of section a is preferably uniform and does not vary. The external diameter of theflexible mandrel 14 over the length of section b does vary in accordance with the invention so that its external cross-sectional dimension or diameter adjacent section a is less than its cross-sectional external dimension or diameter adjacent the right end of section c as viewed in FIG. 1. Conversely, the external cross-sectional dimension or diameter of theflexible mandrel 14 then preferably decreases over the length of section c, as viewed in FIG. 1, so that its external cross-sectional dimension or diameter adjacent the left end of section b is greater than it is adjacent the right end of section d, as viewed in FIG. 1. At this point theflexible mandrel 14 is terminated leaving just the taperedtail 12 of therigid mandrel 10 to be exposed over the length of section d. The internal cross-sectional dimension or diameter of theflexible mandrel 14 tubular sleeve is preferably substantially constant over the length of sections a, b and c because therigid mandrel 10 is substantially cylindrical and, therefore, constant in those sections. - The increasing cross-sectional dimension or diameter of the
flexible mandrel 14 over section b and the decreasing cross-sectional dimension or diameter over section c is an important feature of the invention because it achieves a principal part of the double taper of the molded article of the invention. - The varying tapered sections and cross-sectional dimensions or diameters of the
flexible mandrel 14 may be achieved either by molding the flexible mandrel with these varying dimensions or by sliding a sleeve of the flexible mandrel material over therigid mandrel 10 and then sanding or grinding down the exterior surface of the sleeve toward the ends of the sleeve to achieve the varying cross-sectional dimension or diameter. - In order to form the double tapered molded article A of the invention, the
flexible mandrel 14 is first assembled upon therigid mandrel 10 by slipping it over the conditioned and waxedrigid surface 16 of the rigid mandrel until theend 18 of the flexible mandrel assumes the position spaced slightly from theend 20 of therigid mandrel 10 as seen in FIGS. 1 and 2. - In preferred form once the
flexible mandrel 14 is positioned upon therigid mandrel 10, it will cover and conform to therigid surface 16 of the rigid mandrel, will extend over the lengths of sections a, b and c as shown in FIG. 1, and will terminate before the beginning of section d. Only the taperedtail 12 of therigid mandrel 10 will be present and exposed over the length of section d. Finally, there will be no mandrel over the length of section e, as shown in FIG. 1. - Assembly of the molded article A may now be commenced. This is typically done by wrapping a pre-impregnated cloth or
tape material 22, as depicted in dot and dash in FIGS. 1 and 2, back and forth over the length of the mandrels. However, the impregnated cloth wrapping is preferably terminated at 24 just short of theright end 18 of theflexible mandrel 14 as viewed in FIGS. 1 and 2 to permit the exposure of a short portion of the length of the flexible mandrel to facilitate its removal once the molding operation is completed. - The impregnated cloth or
tape 22 is preferably impregnated with a thermosetting resin, and most preferably an epoxy resin which may be cured by heat. The tape itself may be woven or be fibers of fiberglass, carbon or ceramic in the form of a fabric. Suitable examples of preimpregnated fiberglass cloth or tape include MXB7409/1557 or MXB7409/7576, and of preimpregnatetd unidirectional carbon fiber tape include HYE949b, all available from Cytec Fiberite, Inc. Each of these has a cure temperature of 250° F. - When the wrapping of the resin impregnated cloth or
tape 22 has been completed, it will cover and conform to the exterior surface of theflexible mandrel 14 over the length of section a (except for the small unwrapped portion between theend 18 of the flexible mandrel and theend 24 of the wrap), the entire length of the increasing cross-sectional dimension exterior surface in section b; the entire length of the decreasing cross-sectional dimension exterior surface in section c; over therigid surface 16 of the taperedtail 12 of therigid mandrel 10; and over the length of the short section e where the impregnatedcloth 22 is only wrapped upon itself without the support of any mandrel. - The article thus far assembled is then wrapped preferably with a tight stretch film wrapping26 over its length, and as depicted in dot and dash in FIGS. 1 and 2. The stretch film wrap 26 constrains the resin impregnated
cloth 22 during setting and curing. Because theflexible mandrel 14 is formed of a material which has a high thermal coefficient of expansion and thesurface 16 of therigid mandrel 10 itself is rigid, pressure will be exerted upon the inner surface of the resin impregnatedcloth 22 during curing. Although a tight stretch film wrapping is preferred, other forms of external constraint also may be employed, such as a pressurized external bladder or bag or a two piece female mold clamped in place under pressure over the wrapped resin impregnated tape orcloth 22 to apply external pressure during curing. It will also be appreciated that depending upon the form of exterior constraint which is employed, resins in other more fluid or flowable forms than impregnated into fabrics or tapes may be applied to the mandrels and then cured to form the molded article A of the invention. - The entire assembly, as thus far described, is now heated to a temperature sufficient to cure the resin in the resin impregnated
cloth 22. Once the resin has been cured and set and cools, therigid mandrel 10 may be easily removed from theflexible mandrel 14, as seen in FIG. 3, through the opening which is formed in theend 24 of the article A. Removal of therigid mandrel 10 is simplified because it is of a uniform cross-sectional dimension over most of its length. Where it is not of uniform cross-sectional dimension at its taperedtail 12, its cross-sectional dimension is diminishing which does not impede removal. - Once the
rigid mandrel 10 has been removed, theflexible mandrel 14 may now relax slightly away from theinner wall 28 of thepassage 30 which has been formed by the mandrels during the molding process, as seen in FIG. 4. Furthermore, when theflexible mandrel 14 is pulled to remove it from thepassage 30 in the direction of the arrow as seen in FIG. 4, it may further stretch somewhat which also tends to reduce its cross-sectional dimension or diameter to further simplify the removal of the flexible mandrel from the opening in theend 24 of the article A. Thus, it will be seen that the removal of theflexible mandrel 14 may be easily performed even though the diameter or cross-sectional dimension of the opening and thepassage 30 is less at theend 24 than at a location to the left of theend 24 of thepassage 30 as viewed in FIG. 4. - Although the
flexible mandrel 14 may relax somewhat away from theinner wall 28 ofpassage 30 when therigid mandrel 10 is removed and/or when it is pulled to remove it, it preferably retains sufficient body to generally maintain its original shape and does not just collapse. - As previously mentioned, one such article A which may be molded in accordance with the principles of the present invention, is the shaft of a javelin which is tapered toward each end of the shaft. The method of the present invention makes it possible to form a javelin shaft of a one piece composite polymeric material by molding which was not heretofore possible.
- Once the shaft has been completed, in order to complete the javelin, the tail tip of the shaft at the left end of section e, as viewed in FIG. 1, is preferably cut off to form the tail of the javelin, and the
right end 24 is trimmed as necessary to remove any ragged edges. Ahollow javelin point 32 of steel or aluminum is then press fit onto the taperingend 24 of the javelin shaft A, and ahand grip 34 preferably of wrapped cotton cord, is formed intermediate the ends of the javelin and at approximately the center of gravity of the javelin. - The method of forming the molded composite polymeric one piece article of the present invention is particularly advantageous in the making of a javelin shaft. This is because the competition specifications of a javelin are quite rigid and the double tapers, their sizing and location are advantageously considered in the weight and balance of the javelin, its mass and ability to flex.
- It will be understood that the embodiments of the present invention which have been described are merely illustrative of a few of the applications of the principles of the invention. Numerous modifications may be made by those skilled in the art without departing from the true spirit and scope of the invention.
Claims (30)
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US09/812,933 US6530865B2 (en) | 2001-03-20 | 2001-03-20 | Double tapered article |
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US09/812,933 US6530865B2 (en) | 2001-03-20 | 2001-03-20 | Double tapered article |
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US20020136847A1 true US20020136847A1 (en) | 2002-09-26 |
US6530865B2 US6530865B2 (en) | 2003-03-11 |
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Cited By (4)
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CN100425438C (en) * | 2005-11-09 | 2008-10-15 | 蓝碧儿 | Double layer hardness pen cap production method |
US20090133817A1 (en) * | 2006-06-19 | 2009-05-28 | Patrick Sabaria | Stent manufacturing methods |
US20200306605A1 (en) * | 2019-03-25 | 2020-10-01 | Erick Conrad Friedman | Weight adjustable throwing javelin |
FR3150777A1 (en) * | 2023-07-05 | 2025-01-10 | Latecoere | Geodesic structure with transmission of forces in two perpendicular directions and production method. |
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US20060281593A1 (en) * | 2005-06-09 | 2006-12-14 | Young John N | Clad surface arrow construction |
US8324515B2 (en) | 2007-10-16 | 2012-12-04 | Honeywell International Inc. | Housings for electronic components |
US8388473B2 (en) * | 2008-05-20 | 2013-03-05 | Easton Technical Products, Inc. | Arrow shaft with transition portion |
US7869216B2 (en) | 2008-08-25 | 2011-01-11 | Honeywell International Inc. | Composite avionics chassis |
US9829291B2 (en) | 2010-11-10 | 2017-11-28 | Aldila Golf Corporation | Arrow having multiple exterior diameters and multiple interior diameters |
US8876640B2 (en) | 2010-11-29 | 2014-11-04 | Aldila Golf Corp. | Archery arrow having improved flight characteristics |
US9644927B2 (en) | 2010-11-29 | 2017-05-09 | Aldila Golf Corp. | Archery arrow having improved flight characteristics |
US20150087479A1 (en) * | 2013-09-20 | 2015-03-26 | Juris Terauds | Athletic javelin with maximum moment of inertia |
JP7071276B2 (en) | 2016-04-26 | 2022-05-18 | アプライド メディカル リソーシーズ コーポレイション | Residual stress characteristics of organ model |
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US4404053A (en) * | 1980-02-19 | 1983-09-13 | Victor Saffire | Method of making a javelin |
US5262121A (en) * | 1991-12-18 | 1993-11-16 | Goodno Kenneth T | Method of making and using flexible mandrel |
US5534203A (en) * | 1994-02-09 | 1996-07-09 | Radius Engineering, Inc. | Composite pole manufacturing process for varying non-circular cross-sections and curved center lines |
-
2001
- 2001-03-20 US US09/812,933 patent/US6530865B2/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100425438C (en) * | 2005-11-09 | 2008-10-15 | 蓝碧儿 | Double layer hardness pen cap production method |
US20090133817A1 (en) * | 2006-06-19 | 2009-05-28 | Patrick Sabaria | Stent manufacturing methods |
US20200306605A1 (en) * | 2019-03-25 | 2020-10-01 | Erick Conrad Friedman | Weight adjustable throwing javelin |
US11607592B2 (en) * | 2019-03-25 | 2023-03-21 | Erick Conrad Friedman | Weight adjustable throwing javelin |
FR3150777A1 (en) * | 2023-07-05 | 2025-01-10 | Latecoere | Geodesic structure with transmission of forces in two perpendicular directions and production method. |
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